(b)
For Business Class seats, do these steps:
NOTE: This task applies to BE Aero Millennium 87989 series without transition
zone passenger seats.
1) Tighten the screw on the rear leg track fitting to 60 ±10 in-lb (7 ± 1 N.m).
NOTE: Screw is installed correctly when the screw head is flush with the top of the seat track fitting. 2) Tighten the anti-rattle nut on the forward leg track fitting manually plus 1/4 turn.
XIA 008-011
SUBTASK 25-22-01-420-337
(c) For Economy Class Seats do these steps: NOTE: This task is for Weber 5600 passenger seat. 1) Tighten the screw on the rear leg track fitting to 45 ± 10 in-lb (5.1 ± 1.1 N.m) 2) Tighten the screw on the forward leg track fitting to 45 ± 10 in-lb (5.1 ± 1.1
N.m)
XIA 003-004
SUBTASK 25-22-01-420-335
(d) For Economy Class Seats seats, do these steps to tighten the front and rear seat track fitting fasteners: NOTE: This task is for Recaro 770 passenger seat.
1) Tighten the screw [1] on the rear seat fitting [2] to 80 ± 8 in-lb (9 ± 1 N.m). NOTE: THE TOP SURFACES MUST BE LEVEL TO MAKE SURE THAT THE FITTING IS LOCKED.
2) To tighten the front anti-rattle device [3] do one of these steps:
3) Use the Recaro tool, P/N 046140, and tighten to 53 ± 9 in-lb (6.0 ± 1.0 N.m).
4) Tighten the anti-rattle device manually plus 1/8 to 1/4 turn.
EFFECTIVITY: 003‐004, 008‐011 25-22-01 PAGE 403
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AAR PROPRIETARY - Do not copy without express permission of AAR
XIA 003-004, 008-011
SUBTASK 25-22-01-860-004
(3) FOR AIRPLANES WITH EMERGENCY LIGHTING INSTALLED ON THE SEAT; connect the electrical connectors for the emergency lighting installed on the seat.
SUBTASK 25-22-01-420-053
(4) Connect the electrical connectors for the electrical equipment, if installed.
SUBTASK 25-22-01-420-006
(5) Install the seat track covers.
SUBTASK 25-22-01-860-005
(6) Close the applicable circuit breakers and remove the DO-NOT-CLOSE tags for the seat electrical equipment, if installed.
------------------------- END OF TASK ---------------------------
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B737‐700
SUPPLEMENTAL AIRCRAFT MAINTAINANCE MANUAL
Passenger Seat Installation
Figure 401 (Sheet 1 of 3)/25-22-01-990-801
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AAR PROPRIETARY - Do not copy without express permission of AAR
CLASS DIVIDER HEADER -REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1)
Fixed Class Divider Header Removal,
中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA) 持续适航说明(6)